DE690522C - Device for scaffolding for aircraft manufacture - Google Patents

Device for scaffolding for aircraft manufacture

Info

Publication number
DE690522C
DE690522C DE1938H0155065 DEH0155065D DE690522C DE 690522 C DE690522 C DE 690522C DE 1938H0155065 DE1938H0155065 DE 1938H0155065 DE H0155065 D DEH0155065 D DE H0155065D DE 690522 C DE690522 C DE 690522C
Authority
DE
Germany
Prior art keywords
scaffolding
nipple
threaded
mounting plate
aircraft manufacture
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE1938H0155065
Other languages
German (de)
Inventor
Heinrich Werth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Henschel Flugzeugwerke AG
Original Assignee
Henschel Flugzeugwerke AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Henschel Flugzeugwerke AG filed Critical Henschel Flugzeugwerke AG
Priority to DE1938H0155065 priority Critical patent/DE690522C/en
Application granted granted Critical
Publication of DE690522C publication Critical patent/DE690522C/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Description

Vorrichtung für Baugerüste' für die Flugzeugherstellung Die Erfindung betrifft eine Vorrichtung für Baugerüste für die Flugzeugherstellung nach dem Patent 688 593, bei welcher eine Aufspannplatte durch mehrere an der Aufspannplatte schraubbar angeordnete Gewindenippel an einer Grundplatte parallel zu sich einstellbar vorgesehen und die Grundplatte mittels in die Gewindenippel einschraubbarer Gewindebolzen am Baugerüst befestigt ist.Device for scaffolding 'for aircraft manufacture The invention relates to a device for scaffolding for aircraft manufacture according to the patent 688 593, in which one clamping plate can be screwed through several on the clamping plate arranged threaded nipple provided on a base plate adjustable parallel to itself and the base plate by means of threaded bolts that can be screwed into the threaded nipple Scaffolding is attached.

Die Verbesserung gemäß vorliegender Erfindung besteht darin, daß die Gewindenippel in der am Baugerüst befestigten Grundplatte schraubbar angeordnet sind und die auf den Nippelköpfen aufliegende Aufspannpla.tte mittels durch eine Axialbohrung der Nippel hindurch in die Gewindelöcher der Rufspannplatte einschraubbarer Schrauben befestigt ist.The improvement of the present invention is that the Threaded nipple arranged screwable in the base plate attached to the scaffolding and the clamping plate resting on the nipple heads by means of a Axial bore of the nipple through which can be screwed into the threaded holes of the call clamping plate Screws is attached.

Diese Ausbildung der Vorrichtung ergibt den Vorteil, daß die Gesamtfläche der Rufspannplatte als Arbeitsfläche verwendbar ist, weil vorstehende Schraubenköpfe o. dgl. nicht vorhanden sind. Gleichzeitig ist ein größerer Verstellbereich für die Rufspannplatte erzielt, der der beliebig wählbaren Nippellänge entspricht. Ferner wird bei dem Verstellen der Rufspannplatte die Befestigung der Grundplatte am Baugerüst nicht gelockert, so- daß z. B. bei einer Befestigung in Langlöchern des Baugerüstes keine Änderung der Lage der Vorrichtung am Baugerüst eintreten kann.This design of the device has the advantage that the total area the Rufspannplatte can be used as a work surface, because protruding screw heads o. The like. Are not available. At the same time there is a larger adjustment range for the Rufspannplatte achieved, which corresponds to the freely selectable nipple length. Further the attachment of the base plate to the scaffolding is used when adjusting the clamping plate not loosened, so that z. B. when fastening in elongated holes in the scaffolding no change in the position of the device on the scaffolding can occur.

In der Zeichnung ist ein Ausführungsbeispiel des Erfindungsgegenstandes dargestellt. Es bezeichnet 5 einen Träger des Baugerüstes, an welchem die Grundplatte 7 der Vorrichtung durch eine Schraube 6 befestigt ist. Die Gewindenippel 2 sind in der Grundplatte 7 schraubbar angeordnet und weisen einen verstärkten und für den Angriff eines Schraubenschlüssels entsprechend geformten Kopf io auf, dessen als Kugelfläche ausgebildete Oberseite zur Aufnahme der Rufspannplatte i dient, die entsprechende kugelflächenförmige Ausnehmungen 9 aufweist. Die Gewindenippel 2 sind mit einer durchgehenden glatten Axialbohrung 17 versehen, durch die eine Schraube 18, die einen Kopf i9 hat, geführt ist. Die Schrauben 18 werden in Gewindelöchern 2o der Rufspannplatte i eingeschraubt und bewirken die Befestigung der Platte i an den Gewindenippeln.The drawing shows an exemplary embodiment of the subject matter of the invention shown. It denotes 5 a support of the scaffolding on which the base plate 7 of the device is fastened by a screw 6. The threaded nipples 2 are arranged screwable in the base plate 7 and have a reinforced and for the attack of a wrench correspondingly shaped head io, whose The upper side, designed as a spherical surface, serves to accommodate the ring clamping plate i, which has corresponding recesses 9 in the form of spherical surfaces. The threaded nipple 2 are provided with a continuous smooth axial bore 17 through which one Screw 18, which has a head i9, is guided. The screws 18 are in threaded holes 2o of the Rufspannplatte i screwed in and cause the attachment of the plate i on the threaded nipples.

Claims (2)

PATENTANSPRÜCHE: i. Vorrichtung für Baugerüste für die Flugzeugherstellung mit einer mittels Gewindenippel parallel zu sich einstellbaren Aufbauplatte nach Patent 688 593, dadurch gekennzeichnet, daß die Gewindenippel (2) in der am Baugerüst befestigten Grundplatte (7) schraubbar angeordnet sind und die auf den Nippelköpfen (io) aufliegende Aufbauplatte (i) mittels durch eine Axialbohrung der Nippel (2) hindurch in Gewindelöchern der Aufbauplatte einschraubbarer Schrauben befestigt ist. PATENT CLAIMS: i. Device for scaffolding for aircraft manufacture with a mounting plate that can be adjusted parallel to itself by means of a threaded nipple Patent 688 593, characterized in that the threaded nipple (2) on the scaffolding attached base plate (7) are arranged screwable and on the nipple heads (io) surface mounting plate (i) by means of an axial hole in the nipple (2) fastened through in threaded holes of the mounting plate screw-in screws is. 2. Vorrichtung nach Anspruch i, dadurch gekennzeichnet, daß an der Aufbauplatte (i) kugelflächenförmige Ausnehmungen (9) als Anlage für die Nippel (2) vorgesehen sind.2. Apparatus according to claim i, characterized in that on the mounting plate (i) spherical surface-shaped recesses (9) provided as a system for the nipple (2) are.
DE1938H0155065 1938-03-09 1938-03-09 Device for scaffolding for aircraft manufacture Expired DE690522C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1938H0155065 DE690522C (en) 1938-03-09 1938-03-09 Device for scaffolding for aircraft manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1938H0155065 DE690522C (en) 1938-03-09 1938-03-09 Device for scaffolding for aircraft manufacture

Publications (1)

Publication Number Publication Date
DE690522C true DE690522C (en) 1940-04-27

Family

ID=7182046

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1938H0155065 Expired DE690522C (en) 1938-03-09 1938-03-09 Device for scaffolding for aircraft manufacture

Country Status (1)

Country Link
DE (1) DE690522C (en)

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